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Damage mechanism and evaluation model of compressor impeller remanufacturing blanks: A review

机译:压缩机叶轮再制造坯件的损伤机理及评估模型

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摘要

The theoretical and technological achievements in the damage mechanism and evaluation model obtained through the national basic research program "Key Fundamental Scientific Problems on Mechanical Equipment Remanufacturing" are reviewed in this work. Large centrifugal compressor impeller blanks were used as the study object. The materials of the blanks were FV520B and KMN. The mechanism and evaluation model of ultra-high cycle fatigue, erosion wear, and corrosion damage were studied via theoretical calculation, finite element simulation, and experimentation. For ultra-high cycle fatigue damage, the characteristics of ultra-high cycle fatigue of the impeller material were clarified, and prediction models of ultra-high cycle fatigue strength were established. A residual life evaluation technique based on the "β-H_v-N'' (where β was the nonlinear parameter, H_v was the Vickers hardness, and N was the fatigue life) double criterion method was proposed. For erosion wear, the flow field of gas-solid two-phase flow inside the impeller was simulated, and the erosion wear law was clarified. Two models for erosion rate and erosion depth calculation were established. For corrosion damage, the electrochemical and stress corrosion behaviors of the impeller material and welded joints in H_2S/CO_2 environment were investigated. K_(ISCC) (critical stress intensity factor) and da/dt (crack growth rate, where a is the total crack length and t is time) varied with H_2S concentration and temperature, and their variation laws were revealed. Through this research, the key scientific problems of the damage behavior and mechanism of remanufacturing objects in the multi-strength field and cross-scale were solved. The findings provide theoretical and evaluation model support for the analysis and evaluation of large centrifugal compressor impellers before remanufacturing.
机译:本文对通过国家基础研究计划“机械设备再制造的关键基础科学问题”获得的损伤机理和评估模型的理论和技术成果进行了综述。大型离心压缩机叶轮毛坯被用作研究对象。毛坯的材料是FV520B和KMN。通过理论计算,有限元模拟和实验研究了超高周疲劳,冲蚀磨损和腐蚀破坏的机理和评估模型。针对超高周疲劳的破坏,阐明了叶轮材料的超高周疲劳的特征,建立了超高周疲劳强度的预测模型。提出了一种基于“β-H_v-N”(其中β为非线性参数,H_v为维氏硬度,N为疲劳寿命)双重准则的剩余寿命评估技术,针对冲蚀磨损,流场模拟了叶轮内部的气固两相流场,阐明了磨蚀磨损规律,建立了两种腐蚀速率和腐蚀深度计算模型,针对腐蚀破坏,研究了叶轮材料和焊接件的电化学腐蚀和应力腐蚀行为研究了H_2S / CO_2环境下的接头,K_(ISCC)(临界应力强度因子)和da / dt(裂纹扩展率,a为总裂纹长度,t为时间)随H_2S浓度和温度的变化而变化。通过研究,解决了多强度领域和跨尺度的再制造对象的破坏行为和机理的关键科学问题,为理论和评价工作提供了理论依据。在重新制造之前为大型离心式压缩机叶轮的分析和评估提供德尔支持。

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